Future helicopter requirements dictate need for improved propulsion system in terms of lower specific fuel consumption and mission effective decreases in propulsion system weight; paper shows magnitude of engine improvements which can result from incorporation of advanced technology with particular emphasis on variable turbine applied to regenerated free turbine engine; incorporation and development of high temperature turbine component technology for regenerated and nonregenerated turbine type turboshaft engines is stressed.


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    Title :

    Variable area turbine for future turboshaft engines


    Additional title:

    Am Helicopters Soc -- J


    Contributors:


    Publication date :

    1965


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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